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Aerodynamic characteristics of a delta wing with leading edge swept back 45 degrees, aspect ratio 4, and NACA 65A006 airfoil section.Transonic-bump method

Aerodynamic characteristics of a wing with quarter-chord line swept back 35©�, aspect ratio 6, taper ratio 0.6, and NACA 65A006 airfoil section.Transonic-bump method

Effects of compressibility on lift and load characteristics of a tapered wing of NACA 64-210 airfoil sections up to a Mach number of 0.60

Aerodynamic characteristics of a wing with quarter-chord line swept back 45 degrees, aspect ratio 4, taper ratio 0.3, and NACA 65A006 airfoil section.Transonic-bump method

Published Year

• 1940-1949 (4) *

Subject

• Lift (Aerodynamics) (4)
• Pitching (Aerodynamics) (4) *
• Drag (Aerodynamics) (3)
• Charts, diagrams, etc (2)
• Wind tunnel testing (2)
• Aerodynamics, Transonic (1)
• Aerofoils (1)
• Aerofoils--Testing (1)
• Airplane--Wings, Swept-back (1)
• Airplanes--Fuselage (1)
• Airplanes--WIngs (1)
• Airplanes--Wings (1)
• Airplanes--Wings, Swept-back (1)
• Airplanes--Wings, Triangular (1)

Author

• Sleeman, William C. (2)
• Becht, Robert E. (1)
• Himka, T. (1)
• King, Thomas J. (1)
• Morrison, William D. (1)
• Myers, Boyd C. (1)
• West, F. E. (1)

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